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Pages in category "Single-engined piston aircraft" The following 200 pages are in this category, out of approximately 1,153 total. This list may not reflect recent changes .
The Tomahawk was introduced in 1977 as a 1978 model. The aircraft was in continuous production until 1982 when production ended, with 2,484 aircraft built. The 1981 and 1982 models were designated as the Tomahawk II. They incorporated improved cabin heating and windshield defroster performance, an improved elevator trim system, improved engine ...
AT-802U prototype at Paris Air Show. In response to the United States Air Force's LAAR program and the growing requirement for light counter-insurgency aircraft, [5] Air Tractor developed an armed model, the AT-802U, in 2008, with engine and cockpit armor, a bulletproof windscreen, self-sealing fuel tanks, and structural reinforcements for the carriage of 9,000 pounds (4,100 kg) of payload.
The Bellanca Viking and Super Viking are a series of single-engine, four-seat, high performance, retractable gear aircraft manufactured in the USA during the 1960s and 1970s. The aircraft developed through modifications of classic designs by the aviation pioneer Giuseppe Bellanca. A total of 1,356 Vikings have been produced with most production ...
The Piper PA-18 Super Cub is a two-seat, single-engine monoplane. Introduced in 1949 by Piper Aircraft, it was developed from the PA-11 Cub Special, and traces its lineage back through the J-3 Cub to the Taylor E-2 Cub of the 1930s. In close to 40 years of production, over 10,000 were built. [1]
Quicksilver is a line of single and two-place high wing, single-engine, ultralight aircraft that evolved from weight-shift hang gliders including Bob Lovejoy's High Tailer. The earliest powered version, the Quicksilver C, was created as a self-launching hang glider, designed to allow pilots who lived in the flatlands to be able to self-launch ...
Data from Janes' All The World's Aircraft 1982-83 General characteristics Crew: One Capacity: Five passengers Length: 28 ft 2 in (8.59 m) Wingspan: 36 ft 9 in (11.20 m) Height: 9 ft 8 in (2.95 m) Wing area: 175 sq ft (16.3 m 2) Empty weight: 2,303 lb (1,045 kg) Gross weight: 4,000 lb (1,814 kg) Fuel capacity: 87 US gal (72 imp gal; 330 L) (usable capacity) Powerplant: 1 × Continental Motors ...
Category: Single-engine aircraft. 22 languages. ... Single-engined pusher aircraft (1 C, 1,124 P) S. Single-engined helicopters (1 C) Single-engined piston aircraft ...